Flangeless fuel tank

ABSTRACT

A flangeless fuel tank formed of two interfitted cup-shaped tank halves welded along the overlapping portion of the tank halves. Locating protrusions stamped into each tank half provide registration of the halves prior to welding. Spacing dimples stamped into at least one of the fuel tank halves provide a vent space for escaping gases from vaporized coatings.

BACKGROUND OF THE INVENTION

The present invention relates to a welded flangeless container and morespecifically a steel fuel tank.

The preferred prior art method for manufacturing metal fuel tanks is tolap weld two tank halves along mating circumferential flanges formedinto each. This method suffers in that the flanges, which extend outwardfrom the tank, prohibit the tank body from extending to the full expanseof the opening designed to receive it. The circumference of the fueltank body must be reduced in proportion to the size of thecircumferential flange, thereby placing an undesired limit on the volumeof the fuel tank.

To overcome this disadvantage, prior artisans have attempted to create aflangeless metal fuel tank. One problem in fabricating a flangeless tankis maintaining the two halves in alignment during welding. The top halfwants to drop down "into" or "over" the bottom half-much like a box topon a box. Holding the tops consistently in registration has provendifficult.

A variety of coating materials such as zinc (Zn) are used to protectsheet metal from the hazards of exposure. These coatings generally havea vaporization temperature lower than the temperature necessary to weldthe metal. As a result, the coatings vaporize and the resulting gasexpands during the welding process. The expanding vapors can be trappedin pockets along the weld line or can blow out through the molten metalthereby creating defects along the weld line. In either case, thestrength and leak-tight characteristics of the weld are adverselyaffected. This problem can be overcome by providing externalcommunication with the weld location through the use of spacers orprotrusions stamped along the weld line. The spacers or protrusionsmaintain a gap between the pieces to be welded and allow the expandingvapors to escape without adversely affecting the weld.

While the use of spacers or protrusions may solve the problem posed bythe vaporization of metal coatings, each has shortcomings of its own.Spacers require the additional steps of fabrication and placement.Protrusions, in conjunction with the clamping force, have a tendency tocause the metal to bend or to deform. The clamping pressure causes themetal sheet to pivot at the point of contact between the protrusion andthe adjacent metal sheet.

SUMMARY OF THE INVENTION

The aforementioned problems are solved by the present invention whereina flangeless fuel tank includes locating protrusions to maintain thehalves in registration and spacing dimples to vent the weld area. Thetank halves are positioned by bringing a portion of theircircumferential walls into overlapping disposition such that one of thecircumferential walls receives the other. A gap between the overlappingportions of the two tank halves is maintained by an arrangement ofdimples stamped into at least one of the tank halves. This gap providesa vent space which allows the escape of vaporized metal coatings.Preferably, the dimples are arranged in parallel rows to reduce bendingof the metal under clamping force. To facilitate proper positioning ofthe tank halves, locating protrusions are stamped into thecircumferential wall of at least one tank half. The protrusions are ofsubstantially greater height than the spacing dimples, and define theoverlap area between the two tank halves by contact with the exterioredge of the circumferential wall of the other tank half. Once the tankhalves are positioned in registration, an electromagnetic force appliesthe clamping pressure, and the halves are welded along the overlappingportions.

The locator protrusions and spacing dimples provide both registrationand venting by way of a simple and inexpensive, yet highly effectiveprocess. No additional pieces, such as spacers, are required. Thepresent process permits the practical commercial fabrication of a weldedflangeless fuel tank or other container.

These and other objects, advantages, and features of the presentinvention will be more fully understood and appreciated by reference tothe detailed description of the preferred embodiment and the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a perspective, exploded view of two tank halves to be weldedin accordance with the present invention;

FIG. 2 is a fragmentary perspective view of a portion of the two tankhalves to be welded in accordance with the present invention;

FIG. 3 is a fragmentary sectional assembly view taken along lineIII--III of FIG. 2, showing the overlapping disposition of the two tankhalves;

FIG. 4 is a fragmentary perspective view similar to FIG. 2 showing afirst alternative embodiment of the invention; and

FIG. 5 is a fragmentary perspective view similar to FIG. 2 showing asecond alternative embodiment of the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

A flangeless fuel tank constructed in accordance with a preferredembodiment of the present invention is illustrated in FIG. 1 andgenerally designated 10. The fuel tank 10 is comprised of a lower femalehalf 14 and an upper male 12 tank half, both of which are formed ofzinc-coated sheet metal. The tank halves 12 and 14 are generallycup-shaped and are formed using conventional metal-stamping techniques.All described protrusions and dimples also are stamped into the tankhalves. The halves 12 and 14 each include a bottom wall and acircumferential side wall 16 and 18 respectively. The two tank halves 12and 14 interfit such that the circumferential wall 16 of the male tankhalf 12 is received within the circumferential wall 18 of the femaletank half 14 (See FIG. 3). The circumferential walls 16 and 18 of eachtank half 12 and 14 define an overlap area. Weld lines 40 and 40' on thetwo tank halves are centrally disposed within the overlap area andextend parallel to the exterior edge of the circumferential wall 16 and18. When interfitted the weld lines are aligned and a weld is createdalong the aligned lines.

To facilitate proper alignment of the two tank halves 12 and 14,locating protrusions 20 and 22 are stamped into the circumferential wall16 and 18, respectively, of tank halves 12 and 14 (see FIGS. 2 and 3).When the two tank halves 12 and 14 are interfitted, the peripheral edgeof each circumferential wall 16 and 18 abuts against the protrusions 20and 22 stamped within the other circumferential wall 16 and 18 (See FIG.3). This abutting disposition defines and maintains an area of overlapbetween the two tank halves 12 and 14.

As shown in FIGS. 1 and 2, the locating protrusions 20 and 22 of apreferred embodiment are each comprised of a single row of relativelylarge dimples. In the preferred embodiment, the height of protrusions 20and 22 with 0.042-gauge metal is 0.125 inch. The protrusions 20 stampedinto the male tank half 12 extend toward the exterior of the fuel tank10 to abut against the circumferential wall 18 of the female tank half14 (See FIG. 3). The protrusions 22 stamped into the female tank half 14extend toward the interior of the fuel tank 10 to abut against thecircumferential wall of the male tank half 12 (See FIG. 3). The two rowsof protrusions 20 and 22 run parallel to the exterior edge of thecircumferential wall 16 and 18, and are disposed a substantiallyidentical distance therefrom. This disposition ensures that the twocircumferential walls 16 and 18 will simultaneously contact thecorresponding row of protrusions 20 and 22.

To provide vent space for escaping gases in the welding of these coatedmetals, an arrangement of dimples 30 are stamped into thecircumferential wall 18 of at least one of the tank halves. Asillustrated, all of the dimples 30 are formed in the lower tank half 14.Alternatively, selected simples could be formed in both or either tankhalves. In the preferred embodiment depicted in FIG. 2, the dimples 30are arranged into rows 30a and 30b which run parallel to and adjacentthe weld line 40. Two rows of dimples 30 are included on each side ofthe weld line 40 to provide more than a single line of spacing contactbetween the overlapping portions of the tank halves 12 and 14 in thearea subjected to clamping force. This arrangement decreases thedeformation which results from clamping by reducing the metal's tendencyto pivot and buckle in the area subjected to the clamping force. Thefirst pair of rows 30a is located between the weld line 40 and theexterior edge of the circumferential wall 18. The second pair of rows30b are spaced from the weld line 40 on the side opposite the first tworows 30a. The dimples 30 in the two rows of each pair are offset fromone another, which further reduces metal deformation. The dimples 30 inthe exemplary 0.042-gauge steel are 0.125 inch high.

Once the two tank halves 12 and 14 are properly interfitted such thatthey are supported by the locating protrusions 20 and 22,electromagnetism is used as the clamping force to secure the tank halves12 and 14 for welding. Such clamping is generally well known to thosehaving skill in the welding art. A laser beam welding apparatus (notshown but well known) welds the clamped tank halves 12 and 14 along thealigned weld lines 40 and 40' to create a continuous weld (not shown).After welding is complete, the clamping force is released.

Although not specifically discussed above, the upper tank half mayinclude a hole for receiving a sending unit as known to those skilled inthe art.

A first alternative embodiment of the present invention is illustratedin FIG. 4 and is generally similar to the FIGS. 1-3 embodiment.Identical components are identified by the same designating numeralpreceded by "1" (e.g. 12 becomes 112). The only difference isprotrusions 120 and 122, which are intermittent linear segments. Thesegments extend parallel to the exterior edge of the circumferentialwall 16 and 18 and are linearly aligned. A second alternative embodimentis shown in FIG. 5 and again is generally similar to the FIGS. 1-3embodiment. The locating protrusions 20 and 22 are each comprised of asingle continuous ridge extending around the entire periphery of thetank halves 12 and 14, respectively. These two alternative embodimentsprovide reduced vent space in trade-off for increasingly positiveregistration.

The above descriptions are those of preferred embodiments of theinvention. Various alterations and changes can be made without departingfrom the spirit and broader aspects of the invention as set forth in theappended claims, which are to be interpreted in accordance with theprinciples of patent law, including the Doctrine of Equivalents.

The embodiments of the invention in which an exclusive property orprivilege is claimed are defined as follows:
 1. A flangeless fuel tankcomprised of two fuel tank halves welded along a lap joint wherein atleast one of said tank halves is coated with a material having avaporization temperature lower than the temperature necessary to weldsaid tank halves; each of said two fuel tank halves comprised of abottom wall having a peripheral edge and a circumferential wallextending outward from said peripheral edge of said bottom wall; saidtwo fuel tank halves further defined as a male tank half and a femaletank half in that said circumferential wall of said male tank half isreceived within said circumferential wall of said female tank half,thereby defining an overlap portion between the two tank halves; saidoverlap portion having a weld line disposed longitudinally thereon; saidcircumferential walls having locating protrusions disposed therein suchthat said locating protrusions of said male tank half extend toward theexterior of said flangeless fuel tank and said locating protrusions ofsaid female tank half extend toward the interior of said flangeless fueltank, whereby said overlap portion is defined by the abutment of theexterior edge of said circumferential walls with said locatingprotrusions; at least one of said circumferential walls having anarrangement of dimples coextensive with said overlap portion and ofsubstantially lesser depth than said locating protrusions; saidarrangement of dimples further defined as extending from one of saidcircumferential walls toward the other of said circumferential walls,whereby a uniform distance is maintained between said circumferentialwalls at said overlapping portion to allow any of said coating materialwhich vaporizes during welding to escape from said weld line.
 2. Aflangeless fuel tank as defined in claim 1 wherein said arrangement ofdimples is comprised of four rows of dimples disposed substantiallyparallel to said weld line and being of substantially lesser depth thansaid locating protrusions; said four rows of dimples having a first pairof rows disposed on the same longitudinal side of said weld line and asecond pair of rows of dimples disposed on the longitudinal side of saidweld line opposite said first two rows.
 3. A flangeless fuel tank asdefined in claim 1 wherein said locating protrusions are further definedas a row of dimples disposed substantially parallel to said weld line.4. A flangeless fuel tank as defined in claim 1 wherein said locatingprotrusions are further defined as a row of intermittent dashes disposedsubstantially parallel to said weld line.
 5. A flangeless fuel tank asdefined in claim 1 wherein said locating protrusions are further definedas a continuous trough extending longitudinally around saidcircumferential walls and substantially parallel to said weld line.
 6. Aflangeless fuel tank comprising two cup-shaped halves fabricated ofcoated metal and each including a floor and a peripheral wall integraltherewith, each of said walls terminating in an edge, said wallsinterfitting to form said tank, at least one of said walls includingintegral locator protrusions, the edge of said other wall engaging saidprotrusions to provide registration between said tank halves, at leastone of said walls including integral spacer dimples engaging the otherof said walls to define a vent space therebetween, whereby any gasesgenerated during welding may escape through said vent space, said tankhalves being welded together in the proximity of said dimples.
 7. A fueltank as defined in claim 6 wherein both of said walls include saidintegral locator protrusions.
 8. A fuel tank as defined in claim 6wherein the height of said locator protrusions is greater than theheight of said spacer dimples.
 9. A flangeless container comprising:afirst cup-shaped container half having a peripheral side wallterminating in an edge; a second cup-shaped container half fitted withinsaid first container half and having a peripheral side wall terminatingin an edge; registration means integrally formed in at least one of saidcontainer halves for registering said container halves when interfitted,the edge of the other container half engaging said registration meanswhen said container halves are interfitted; spacer means integrallyformed in at least one of said container halves for providing a ventspace between said side walls, said vent space allowing any gasesgenerated during welding to escape from between said side walls; andjoining means for permanently interconnecting said container halves. 10.A container as defined in claim 9 wherein said registration meanscomprises a plurality of protrusion arranged in a line.
 11. A containeras defined in claim 9 wherein said registration means comprises acontinuous linear protrusion.
 12. A container as defined in claim 9wherein both of said halves are fabricated of coated metal and saidjoining means comprises a weld.